AD/SC7/17 - Outer Flap - Replacement of Lifed Items and Reinforcement of Flap Structure

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B06792 In force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Short SC7 (Skyvan) Series Aeroplanes

 

AD/SC7/17 Outer Flap - Replacement of Lifed Items

and Reinforcement of Flap Structure

Applicability: All Skyvan series 3, 3A and 3M. Document:  Short SB No. 57-62.

Compliance: As detailed in the requirement document.


7/80

 

Background: Retirement of hinge arms and operating arms, and reinforcement of the flap structure, are required as part of the life extension modification and to ensure the continued airworthiness of the flaps.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.